A piloted flight simulator called the Ice Contamination Effects Flight Training Device (ICEFTD), which uses low cost desktop components and a generic cockpit replication is being developed. The purpose of this device is to demonstrate the effectiveness of its use for training pilots to recognize and recover from aircraft handling anomalies that result from airframe ice formations. High-fidelity flight simulation models for various baseline (non-iced) and iced configurations were developed from wind tunnel tests of a subscale DeHavilland DHC-6 Twin Otter aircraft model. These simulation models were validated with flight test data from the NASA Twin Otter Icing Research Aircraft, which included the effects of ice on wing and tail stall characteristics. These simulation models are being implemented into an ICEFTD that will provide representative aircraft characteristics due to airframe icing. Scenario-based exercises are being constructed to give an operational-flavor to the simulation. Training pilots will learn to recognize iced aircraft characteristics from the baseline, and will practice and apply appropriate recovery procedures to a handling event.
Development and Utility of a Piloted Flight Simulator for Icing Effects Training
2003
18 pages
Report
No indication
English
Aircraft , Test Facilities & Equipment , Aircraft icing , Flight simulation , Flight training , Wind tunnel tests , Flight simulators , Aviation safety , Aircraft models , Aircraft design , Propulsion system performance , Aircraft pilots , Real time operation , DeHavilland aircraft , Accident reduction
DEVELOPMENT AND UTILITY OF A PILOTED FLIGHT SIMULATOR FOR ICING EFFECTS TRAINING
British Library Conference Proceedings | 2003
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